Garrett TPE331
| TPE331 / T76 | |
|---|---|
_TPE331-14.jpg) | |
| TPE331-14 | |
| Type | Turboprop |
| National origin | United States |
| Manufacturer | Garrett AiResearch Honeywell Aerospace |
| First run | 1960 |
| Major applications | Fairchild Swearingen Metroliner Mitsubishi MU-2 Rockwell Turbo Commander |
| Number built | 13,000+[1] |
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The Garrett AiResearch TPE331 is a turboprop engine originally designed and manufactured by Garrett AiResearch, and produced by Honeywell Aerospace since 1999 after that company acquired Garrett. The TPE331 family includes 18 models and 106 configurations; the engines range from 575 to 1650 shaft horsepower.[2][3][4] The military version is designated the T76.
Design and development
The TPE331 originated in 1961 as a gas turbine (the "331") to power helicopters.[5] It first went into production in 1963.[6] More than 700 had been shipped by the end of 1973.[7] It was designed to be both a turboshaft (TSE331) and a turboprop (TPE331), but the turboshaft version never went into production; however, over 14,000 TPE331s have been sold since the first engine was produced in 1963, installed on the Aero Commander in 1964 and put into production on the Aero Commander Turbo Commander in June 1965.[8]
Applications
- Aero/Rockwell Turbo Commander 680/690/840/960/1000
- Antonov An-38
- Ayres Thrush
- BAe Jetstream 31/32
- BAe Jetstream 41
- Beechcraft Model 18Note
- Beech B100 King Air
- CASA C-212 Aviocar
- Cessna 441 Conquest II
- Cessna SkymasterNote
- Comp Air 9
- Conroy Stolifter
- de Havilland DoveNote
- Dornier Do 228
- Fairchild Swearingen Metroliner
- FMA IA 58 PucaráNote
- General Atomics MQ-9 Reaper
- Grob G 520
- Grumman Ag CatNote
- Grumman S-2 TrackerNote
- HAL HTT-40
- Handley Page Jetstream
- Kestrel K-350
- Marsh S-2F3AT Turbo TrackerNote
- Mitsubishi MU-2
- North American Rockwell OV-10 Bronco
- PAC FletcherNote
- Pilatus/Fairchild PC-6C Turbo-Porter
- Piper Cheyenne 400
- Short SC.7 Skyvan
- Short Tucano
- Swearingen Merlin
- Volpar Model 4000Note
Specifications (TPE331-43A)
Data from Canadian Museum of Flight.[9]
General characteristics
- Type: Single-shaft turboprop with integral gearbox
- Length: 46 in (1168 mm),
- Diameter: 21 in (533 mm)
- Dry weight: 336 lb (153 kg)
Components
- Compressor: Two-stage centrifugal
- Combustors: Reverse annular
- Turbine: Three-stage axial
Performance
- Maximum power output: 575 hp (429 kW)
- Power-to-weight ratio: 1.71 hp/lb (2.8 kW/kg)
See also
- Related lists
Note
^ These aircraft were fitted with TPE-331s as a modification to replace their original engines
References
- ↑ Product page Honeywell. Accessed: 29 August 2014.
- ↑ "Honeywell Aerospace TPE331 Spec Chart" Honeywell. Accessed: 29 August 2014.
- ↑ Archived September 8, 2010 at the Wayback Machine
- ↑ "TPE331-14 Turboprop Engine" Honeywell. Accessed: 29 August 2014.
- ↑ William A. Schoneberger and Robert R. H. Scholl, Out of Thin Air: Garrett's First 50 Years, Phoenix: Garrett Corporation, 1985 (ISBN 0-9617029-0-7), pp. 174-5.
- ↑ Canadian Museum of Flight, "Garrett TPE331"
- ↑ Schoneberger and Scholl, p. 203.
- ↑ Leyes, p. 725
- ↑ Canadian Museum of Flight "Garrett TPE331"
- Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. ISBN 0-7509-4479-X.
External links
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Wikimedia Commons has media related to Garrett TPE331. |
- TPE 331 Cost Protection Programs
- TPE 331 Engine Conversions
- Power and fuel flow versus altitude and speed, for version 10. (Archive)
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